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Cockpit Controls (side-stick controllers and levers): SKF Aerospace.
HONEYWELL AEROSPACE, Glendale, AZ, USA February 2005 – present
System Safety Engineer in Avionics and Flight Controls – Consultant (telework)
Produced the Fault Tree Analysis (FTA) for the primary flight controls of the Boeing 787 Fly-By-
Wire system Flight Control Electronic (FCE), which also comprises the autoflight function.
Wrote associated FCE System Safety Analysis (SSA) documentation.
Helped writing FCE system safety guidelines and plans.
Wrote Preliminary System Safety Analysis (PSSA) on related Honeywell research activities for
advanced fault tolerant Fly-By-Wire systems (Digital Flight Control System (DFCS) project with
NASA).
Wrote System Safety Analysis (SSA) for the Honeywell KSG7200 Air Data Attitude Heading
Reference System (ADAHRS) airborne on Dassault F7X and Pilatus PC12 planes.
Produced the Pilatus PC12 Preliminary Common Mode Analysis (PCMA) of the Honeywell EPIC
Automatic Flight Control System (AFCS).
Updated the System Safety Analysis (SSA) previously created for Primus EPIC AFCS and ACAC
ARJ21.
SMITHS AEROSPACE (now GE Aviation) @ BOEING, Everett, WA, USA January 2005 – July 2005
System Safety Engineer for the Boeing 787 Landing Gear Control System
Produced the Preliminary System Safety Analyses (PSSA) for the Boeing 787 Brake System and
Nose Wheel Steering.
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HONEYWELL AEROSPACE, Glendale, AZ, USA August 2001 – July 2003
System Safety Engineer in Avionics and Flight Controls February 2004 – January 2005
Responsible for the production of the Preliminary System Safety Analysis for the fly-by-wire
controls of the ARJ21 regional jet of China’s AVIC I Commercial Aircraft Co. (ACAC).
Responsible for the production of certification documentation: System Safety Analyses (SSA)
and/or Common Mode Analyses (CMA) on the Primus EPIC AFCS for one helicopter
(AgustaWestland AW139) and the following fixed wing aircrafts:
- Embraer ERJ170/175/190/195,
- Dornier Do728 (discontinued),
- Gulfstream G500, G550,
- Dassault Falcon F900EX EASy, F2000 EASy, F7X,
- Raytheon Hawker 4000 Horizon,
- Cessna Citation Sovereign.
The AFCS is highly integrated and typically provides the following functions: autopilot, flight
director, yaw damper, stall warning & stall protection, auto-throttle, pitch autotrim, and Mach trim.
Wrote safety documentation to FAA / EASA system safety regulation (FAR/JAR 25.1309), using
guidance provided by SAE ARP-4761, and SAE ARP-4754.
Derived software and hardware design assurance levels as per RTCA DO-178B and RTCA DO-
254 to support design activities.
Used Matlab Simulink to analyze control laws and propose design improvements, when required.
BOMBARDIER AEROSPACE, Montréal, Canada September 2000 - August 2001
System Safety, Reliability and Maintainability Engineer
System Safety Engineer, responsible in charge of the secondary flight controls (Pitch trim /
Horizontal Stabilizer, Spoilers, Flaps) and the electrical power generation system for the
Continental Business Jet.
Responsible for the production or review of the following Safety documentation:
- Fault Tree Analysis (FTA),
- System Safety Analysis (SSA),
- Failure Mode Effect and Criticality Analysis (FMECA),
- Functional Hazard Analysis (FHA),
- Fire Hazard Analysis,
Involved with Airworthiness Authorities (Transport Canada) regarding the Safety demonstration of
Airworthiness as per JAR/FAR Part 25 (essentially § 25.1309) for the above systems.
Co-ordinate Safety activities with partners in Europe and in U.S. (Moog, E.C.E, Liebherr).
SEXTANT AVIONIQUE (now THALES), Toronto, Canada January 1997 - February 2000
Avionics System Safety & Reliability Engineer
Responsible for Safety & Reliability certification of the avionics suite on the Bombardier
Aerospace DASH 8Q400 regional Turboprop aircraft (more than 100 LRUs including the
following flight controls: Stall Protection System and Autopilot).
Negotiated with Bombardier and Transport Canada (TCA) with regard to Safety & Reliability
contractual requirements and Safety guidelines.
Produced most of the Avionics Safety & Reliability documentation from the preliminary design to
the final certification (e.g. system FMECA, Software Safety Level Assessment, Fault Tree
Analysis and System Safety Analysis, MMEL consolidation, Dispatch Analysis, etc.).
Presented analysis results to the Airworthiness Authorities (Transport Canada) or their
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